Russian Aviation Museum

Light 2-seater hydroplane, designed and tested at Experimental Design Bureau of Flying Vehicles of the Samara Aerospace University (former KuAI). From the very beginning project was developed in compliance with the International Airworthiness Standards
for light aircraft.

If necessary, wheel or ski landing gear may be installed. Possible applications are:
  - Ecological monitoring
  - Forest patrol
  - Aerial photography
  - Pipeline patrol
  - Power line patrol
  - Border patrol
  - Training
  - Tourism, leisure


Type S-202
Function Light hydroplane
Year 1995
Crew 1+1
Powerplant (2)
Type RMZ-640 / Rotax 503-1 V
Power 30hp / 45hp
Size (m)
Length 7.0
Wingspan 12.0
Wing area ?m2
Weights (kg) and loads
Empty 330 / 330
Takeoff 550 / 580
Power load (kg/hp) 9.17 / 6.44
Speed (km/h)
Maximum 135 / 160
Cruising 110 / 130
Landing 60 / 60
Takeoff (m)
Water 250 / 150
Land 150 / 100
Range (km)
Maximum 450 / 600
g-Load +4.5 -2.25
Airframe resource 3000h